Zobrazeno 1 - 10
of 117
pro vyhledávání: '"Yasumasa WATANABE"'
Publikováno v:
Aerospace, Vol 6, Iss 3, p 35 (2019)
This study considers the effect of an electric discharge on the flow structure near a 19.4° compression ramp in Mach-2 supersonic flow. The experiments were conducted in the supersonic wind tunnel SBR-50 at the University of Notre Dame. The stagnati
Externí odkaz:
https://doaj.org/article/2b700c0e48784511b980ef03a9cb216e
Autor:
Kazuhiko YAMADA, Takahiro MORIYOSHI, Kazushige MATSUMARU, Hiroki KANEMARU, Takahiro ARAYA, Kojiro SUZUKI, Osamu IMAMURA, Daisuke AKITA, Yasunori NAGATA, Yasumasa WATANABE
Publikováno v:
Transactions of the Japan Society of Aeronautical & Space Science; 2024, Vol. 67 Issue 4, p224-233, 10p
Publikováno v:
TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, AEROSPACE TECHNOLOGY JAPAN. 19:735-743
Publikováno v:
AIAA SCITECH 2022 Forum.
Publikováno v:
AIAA AVIATION 2021 FORUM.
Publikováno v:
AIAA Scitech 2020 Forum.
Publikováno v:
TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, AEROSPACE TECHNOLOGY JAPAN. 16:420-426
Publikováno v:
Journal of Flow Control, Measurement & Visualization. :136-151
The impact and penetration of a projectile in a particle-laden space, which are expected to have frequently occurred during the formation of the solar system and will occur in the case of an impact probe for future planetary exploration, were experim
Autor:
Sergey B. Leonov, Yasumasa Watanabe
Publikováno v:
AIAA Aviation 2019 Forum.
Publikováno v:
Aerospace
Volume 6
Issue 3
Aerospace, Vol 6, Iss 3, p 35 (2019)
Volume 6
Issue 3
Aerospace, Vol 6, Iss 3, p 35 (2019)
This study considers the effect of an electric discharge on the flow structure near a 19.4°
compression ramp in Mach-2 supersonic flow. The experiments were conducted in the supersonic wind tunnel SBR-50 at the University of Notre Dame. The s
compression ramp in Mach-2 supersonic flow. The experiments were conducted in the supersonic wind tunnel SBR-50 at the University of Notre Dame. The s